钢材标准-SAE AMS 5662M-2004镍基高温合金[1]._pdf
AMS5662
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18FeConsumable Electrode or Vacuum Induction Melted1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable(Composition similar to UNS N07718)1.SCOPE:1.1Form:This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.1.2Application:These products have been used typically for parts requiring high resistance to creep and stress-rupture up to 1300 °F (704 °C) and oxidation resistance up to 1800 °F (982 °C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.2.APPLICABLE DOCUMENTS:The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent supplied herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply.AEROSPACE MATERIALSPECIFICATIONAMS 5662MIssued 1965-09Revised 2004-07Superseding AMS 5662LReaffirmed 2009-06SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright © 2009 SAE InternationalAll rights reserved. No part o f this publicatio n may be repro duced, sto red in a retrieval system o r transmitted, in any fo rm o r by any means, electro nic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA)SAE values your input. To provide feedback--`,,```,,,,````-`-`,,`,,`,`,,`---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\2.1SAE Publications:Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or .AMS 2261Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS 2269Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt AlloysAMS 2371Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings AMS 2750PyrometryAMS 2806Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS 2808Identification, ForgingsAMS 7490Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel, or Cobalt Alloys, or Precipitation-Hardenable Alloys ARP1313Determination of Trace Elements in High-Temperature Alloys2.2ASTM Publications:Available from ASTM, 100 Barr Harbor Drive, P .O. Box C700, West Conshohocken, PA 19428-2959 or .ASTM E 8Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 10Brinell Hardness of Metallic MaterialsASTM E 21Elevated Temperature Tension Tests of Metallic Materials ASTM E 103Rapid Indentation Hardness Testing of Metallic Materials ASTM E 112Determining Average Grain SizeASTM E 139Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E 292Conducting Time-for-Rupture Notch Tension Tests of MaterialsASTM E 354Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys3.TECHNICAL REQUIREMENTS: 3.1Composition:Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, by the methods of ARP1313 for lead, bismuth, and selenium, or by other analytical methods acceptable to purchaser.--`,,```,,,,````-`-`,,`,,`,`,,`---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\3.1.1Determination not required for routine acceptance.3.1.2Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269.3.2Melting Practice:Alloy shall be multiple melted using consumable electrode practice in the remelt cycle or shall be induction melted under vacuum. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.3.3Condition:The product shall be supplied in the following condition:3.3.1Bars: Hot or cold finished, solution heat treated, and descaled except as specified in 3.3.1.1 and 3.3.1.2.3.3.1.1Hot finished round bars shall be ground or turned; all other hot finished bars shall be as hot finished.TABLE 1 - CompositionElementmin maxCarbon -- 0.08Manganese -- 0.35Silicon-- 0.35Phosphorus -- 0.015Sulfur-- 0.015Chromium 17.0021.00Nickel50.0055.00Molybdenum2.803.30Columbium (Niobium)4.755.50Titanium 0.65 1.15Aluminum 0.20 0.80Cobalt-- 1.00Tantalum (3.1.1)-- 0.05Boron -- 0.006Copper -- 0.30Lead -- 0.0005 (5 ppm)Bismuth -- 0.00003 (0.3 ppm)Selenium -- 0.0003 (3 ppm)Ironremainder//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\3.3.1.2Cold finished round bars shall be ground or as cold finished; all other cold finished bars shall beas cold finished.3.3.2Forgings and Flash Welded Rings: Solution heat treated and descaled.3.3.2.1Flash welded rings shall not be supplied unless specified or permitted on purchaser’s partdrawing. When supplied, rings shall be manufactured in accordance with AMS 7490.3.3.3Stock for Forging, Flash Welded Rings, or Heading: As ordered by the forging, flash welded ring,or heading manufacturer.3.4Heat Treatment:Bars, forgings, and flash welded rings shall be solution heat treated by heating to a temperature within the range 1725 to 1850 °F (941 to 1010 °C), holding at the selected temperature within ±25 °F (±14 °C) for a time commensurate with cross-sectional thickness, and cooling at a rate equivalent to an air cool or faster. Pyrometry shall be in accordance with AMS 2750.3.4.1If forgings are not to be machined all over, heat treatment shall be performed in a suitableprotective atmosphere or, when permitted by purchaser, a suitable protective coating may beapplied to the forgings in lieu of using a protective atmosphere.3.5Properties:The product shall conform to the following requirements:3.5.1Bars, Forgings, and Flash Welded Rings:3.5.1.1As Solution Heat Treated:3.5.1.1.1Hardness: Shall be not higher than 277 HB, or equivalent (See 8.2), determined in accordancewith ASTM E 10 or ASTM E 103.3.5.1.1.2Average Grain Size: Shall be as follows, determined by the comparative method ofASTM E 112. In case of disagreement, the intercept (Heyn) procedure shall be used.3.5.1.1.2.1Bars and flash welded rings under 9 square inches (58 cm2) in cross-sectional area shallexhibit an average grain size of ASTM No. 5 or finer. Up to 20% of the cross section of theproduct may have an average grain size of ASTM No. 3 to 5, determined by the interceptmethod of ASTM E 112, due to the presence of nonrecrystallized grains.3.5.1.1.2.2Bars and flash welded rings 9 to 50 square inches (58 to 323 cm2), inclusive, in cross-sectional area and all forgings shall exhibit an average grain size of ASTM No. 4 or finer. Upto 20% of the product cross section may have an average grain size of ASTM No. 2 to 4,determined by the intercept method of ASTM E 112, due to the presence of nonrecrystallized grains.--` , , ` ` ` , , , , ` ` ` ` -` -` , , ` , , ` , ` , , ` ---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\3.5.1.1.3Microstructure: Product shall be free of Laves phase. Banding of acicular phase and amount ofacicular phase shall conform to standards acceptable to purchaser.3.5.1.2Response to Heat Treatment: Product, 5 inches (127 mm) and under in nominal diameter orleast distance between parallel sides, shall meet the requirements of 3.5.1.2.1, 3.5.1.2.2, and3.5.1.2.3 after being precipitation heat treated by heating to 1325 °F ± 15 (718 °C ± 8), holding atheat for not less than eight hours, cooling at a rate of 100 °F ± 15 (56 °C ± 8) degrees per hour to 1150 °F ± 15 (621 °C ± 8), holding at 1150 °F ± 15 (621 °C ± 8) for not less than eight hours, and cooling in air. Instead of the 100 °F (56 °C) degrees per hour cooling rate to 1150 °F ± 15(621 °C ± 8), product may be furnace cooled at any rate provided the time at 1150 °F ± 15(621 °C ± 8) is adjusted to give a total precipitation heat treatment time of not less than 18 hours.3.5.1.2.1Tensile Properties:3.5.1.2.1.1At Room Temperature: Shall be as shown in Table 2, determined in accordance withASTM E 8 or ASTM E 8M.TABLE 2A - Minimum Room Temperature Tensile Properties, Inch/Pound UnitsSpecimen OrientationTensileStrengthksiYield Strengthat 0.2% OffsetksiElongationin 4D%Reduction ofArea%Longitudinal1851501215 Long-Transverse(Forgings)1801501012Transverse(Bars)180150 68 TABLE 2B - Minimum Room Temperature Tensile Properties, SI UnitsSpecimen OrientationTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongationin 4D%Reduction ofArea%Longitudinal127610341215 Long-Transverse(Forgings)124110341012Transverse (Bars)12411034 6 8--`,,```,,,,````-`-`,,`,,`,`,,`---3.5.1.2.1.2AT 1200 °F (649 °C): Shall be as specified in Table 3, determined in accordance withASTM E 21 on specimens heated to 1200 °F ± 5 (649 °C ± 3), held at heat for not less than 20 minutes before testing, and tested at 1200 °F ± 5 (649 °C ± 3).3.5.1.2.1.3Longitudinal requirements of 3.5.1.2.1.1 and 3.5.1.2.1.2 apply to specimens taken with the axis approximately parallel to the grain flow, to specimens taken in the radial direction and in the tangential direction at the rim of disc forgings, and to specimens taken in thecircumferential direction from flash welded rings. All other specimens shall be considered to be in the transverse direction.3.5.1.2.1.4Transverse tensile properties apply only to product from which a tensile specimen not less than 2.50 inches (63.5 mm) long can be obtained.3.5.1.2.1.5Specific locations of specimens from forgings and flash welded rings shall be as agreed upon by purchaser and vendor.TABLE 3A - Minimum Tensile Properties at 1200 °F, Inch/Pound Units Specimen Orientation Tensile Strength ksi Yield Strength at 0.2% OffsetksiElongation in 4D %Reduction ofArea %Longitudinal 1451251215Long-Transverse (Forgings)1401251012Transverse (Bars)140125 6 8TABLE 3B - Minimum Tensile Properties at 649 °C, SI Units Specimen Orientation Tensile Strength MPa Yield Strength at 0.2% OffsetMPaElongation in 4D %Reduction ofArea %Longitudinal 10008621215Long-Transverse (Forgings) 9658621012Transverse (Bars)965862 6 8--`,,```,,,,````-`-`,,`,,`,`,,`---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\3.5.1.2.2Hardness: Shall be not lower than 331 HB, or equivalent (See 8.2), determined in accordancewith ASTM E 10 or ASTM E 103. Product shall not be rejected on the basis of hardness if thetensile property requirements of 3.5.1.2.1.1, determined on specimens taken from the samesample as that with nonconforming hardness or from another sample with similarnonconforming hardness, are acceptable.3.5.1.2.3Stress-Rupture Properties at 1200 °F (649 °C): Shall be as follows; testing of notchedspecimens and of combination smooth-and-notched specimens shall be performed inaccordance with ASTM E 292 and testing of smooth specimens shall be performed inaccordance with ASTM E 139:3.5.1.2.3.1 A standard cylindrical combination smooth-and-notched specimen conforming toASTM E 292, maintained at 1200 °F ± 3 (649 °C ± 2) while a load sufficient to produce aninitial axial stress of 100 ksi (689 MPa) or higher is applied continuously, shall not rupture inless than 23 hours. The test shall be continued to rupture without change of load. Ruptureshall occur in the smooth section and elongation of this section after rupture, measured atroom temperature, shall be not less than 4% in 4D for product 5.0 inches (127 mm) andunder in nominal diameter or distance between parallel sides.3.5.1.2.3.2As an alternate procedure, separate smooth and notched specimens, machined fromadjacent sections of the same piece, with gage sections conforming to the respectivedimensions shown in ASTM E 292 may be tested individually under the conditions of3.5.1.2.3.1. The smooth specimen shall not rupture in less than 23 hours and elongationafter rupture, measured at room temperature, shall be as specified in 3.5.1.2.3.1. Thenotched specimen shall not rupture in less time than the companion smooth specimen butneed not be tested to rupture.3.5.1.2.3.3The tests of 3.5.1.2.3.1 and 3.5.1.2.3.2 may be conducted using incremental loading. In suchcase, the load required to produce an initial axial stress of 100 ksi (689 MPa) or higher shallbe used to rupture or for 23 hours, whichever occurs first. After the 23 hours and at intervalsof 8 hours minimum, thereafter, the stress shall be increased in increments of 5.0 ksi (34.5MPa). Time to rupture, rupture location, and elongation requirements shall be as specified in3.5.1.2.3.1.3.5.1.3After Re-solution and Precipitation Heat Treatment: The product shall meet the requirements of3.5.1.2.1, 3.5.2.1.2.2, and 3.5.1.2.3 after being re-solution heat treated by heating to --`,,```,,,,````-`-`,,`,,`,`,,`---1750 °F ± 25 (954 °C ± 14), holding at heat for not less than 60 minutes, and cooling at a rateequivalent to an air cool or faster and precipitation heat treated as in 3.5.1.2.3.5.2Forging Stock: When a sample of stock is forged to a test coupon, heat treated as in 3.4 and3.5.1.2, specimens taken from the heat treated coupon shall conform to the requirements of3.5.1.2.1, 3.5.1.2.2, and 3.5.1.2.3. If specimens taken from the stock after heat treatment as in 3.4and 3.5.1.2 conform to the requirements of 3.5.1.2.1, 3.5.1.2.2, and 3.5.1.2.3, the tests shall be accepted as equivalent to tests of a forged coupon. Stock shall also meet these requirements after solution heat treatment and re-solution and precipitation heat treatment as in 3.5.1.3.3.5.3Stock for Flash Welded Rings or Heading: Specimens taken from the stock after heat treatment asin 3.4 and 3.5.1.2 shall conform to the requirements of 3.5.1.2.1, 3.5.1.2.2, and 3.5.1.2.3.3.6Quality:The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product.3.6.1Grain flow of die forgings, except in areas which contain flash-line end grain, shall follow thegeneral contour of the forgings showing no evidence of reentrant grain flow.3.7Tolerances:Bars shall conform to all applicable requirements of AMS 2261.4.QUALITY ASSURANCE PROVISIONS:4.1Responsibility for Inspection:The vendor of the product shall supply all samples for vendor’s tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform anyconfirmatory testing deemed necessary to ensure that the product conforms to specifiedrequirements.4.2Classification of Tests:4.2.1Acceptance Tests: The following requirements are acceptance tests and shall be performed oneach heat or lot as applicable.4.2.1.1Composition (3.1) of each heat.4.2.1.2Hardness (3.5.1.1.1) and average grain size (3.5.1.1.2) of each lot of bars, forgings, and flashwelded rings as solution heat treated.4.2.1.3Room-temperature tensile properties (3.5.1.2.1.1), hardness (3.5.1.2.2), and stress-ruptureproperties (3.5.1.2.3) of each lot of bars, forgings, and flash welded rings after precipitation heattreatment.4.2.1.4Microstructure (3.5.1.1.3) of each lot.4.2.1.5 Tolerances (3.7) of bars.4.2.2Periodic Tests: The following requirements are periodic tests and shall be performed at afrequency selected by the vendor unless frequency of testing is specified by purchaser:4.2.2.1Tensile properties at 1200 °F (649 °C) (3.5.1.2.1.2) of bars, forgings, and flash welded rings afterprecipitation heat treatment.--` , , ` ` ` , , , , ` ` ` ` -` -` , , ` , , ` , ` , , ` ---AMS 5662M SAE AMS 5662M4.2.2.2Tensile Properties (3.5.1.2.1), hardness (3.5.1.2.2), and stress-rupture properties (3.5.1.2.3) of bars, forgings, and flash welded rings after resolution and precipitation heat treatment (3.5.1.3).4.2.2.3Ability of forging stock (3.5.2) and of stock for flash welded rings or heading (3.5.3) to develop required properties.4.2.2.4Grain flow (3.6.1) of die forgings.4.3Sampling and Testing: Shall be as follows:4.3.1Bars, Flash Welded Rings, and Stock for Forging, Flash Welded Rings, or Heading: In accordance with AMS 2371.4.3.2Forgings: In accordance with AMS 2374.4.4Reports:4.4.1The vendor of bars, forgings, and flash welded rings shall furnish with each shipment a report showing the results of tests for chemical composition of each heat and the results of tests on each lot to determine conformance to the other acceptance test requirements. This report shall include the purchase order number, heat and lot numbers, AMS 5662M, solution heat treatmenttemperature used, size, and quantity. If forgings are supplied, the part number and the size and melt source of stock used to make the forgings shall also be included.4.4.2The vendor of stock for forging, flash welded rings, or heading shall furnish with each shipment a report showing the results of tests for chemical composition of each heat. This report shall include the purchase order number, heat number, AMS 5662M, size, and quantity.4.5Resampling and Retesting: Shall be as follows:4.5.1Bars, Flash Welded Rings, and Stock for Forgings, Flash Welded Rings, or Heading: In accordance with AMS 2371.4.5.2Forgings: In accordance with AMS 2374.5.PREPARATION FOR DELIVERY: 5.1Sizes:Except when exact lengths or multiples of exact lengths are ordered, straight bars will be acceptable in mill lengths of 6 to 24 feet (1.8 to 7.3 m) but not more than 25% of any shipment shall be supplied in lengths of 6 to 9 feet (1.8 to 2.7 m) except that for bars weighing over 25 pounds per foot (37 kg/m), short lengths down to 2 feet (610 mm) may be supplied.--`,,```,,,,````-`-`,,`,,`,`,,`---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\AMS 5662M SAE AMS 5662M5.2Identification:Shall be as follows:5.2.1Bars: In accordance with AMS 2806.5.2.2Forgings: In accordance with AMS 2808.5.2.3Flash Welded Rings and Stock for Forging, Flash Welded Rings, or Heading: As agreed upon bypurchaser and vendor.5.3Packaging:The product shall be prepared for shipment in accordance with commercial practice and incompliance with applicable rules and regulations pertaining to the handling, packaging, andtransportation of the product to ensure carrier acceptance and safe delivery.6.ACKNOWLEDGMENT:A vendor shall mention this specification number and its revision letter in all quotations and whenacknowledging purchase orders.7.REJECTIONS:Product not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8.NOTES:8.1 A change bar ( l ) located in the left margin is for the convenience of the user in locating areas wheretechnical revisions, not editorial changes, have been made to the previous issue of this specification.An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revisions. Change bars and (R) are not used in original publications, nor inspecifications that contain editorial changes only.8.2Hardness conversion tables for metals are presented in ASTM E 140.8.3Terms used in AMS are clarified in ARP1917.8.4Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary;dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.--`,,```,,,,````-`-`,,`,,`,`,,`---AMS 5662M SAE AMS 5662M - 11 -8.5Purchase documents should specify not less than the following:AMS 5662M Form and size or part number of product desiredQuantity of product desiredSpecific location of tensile specimens from forgings and flash welded rings (See 3.5.1.2.1.5).8.6Key Words:Solution heat treated, precipitation-hardenable, bars, forgings, rings, stress-rupture, grain size, microstructure, UNS N07718PREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “F”Copyright SAE InternationalProvided by IHS under license with SAENot for Resale No reproduction or networking permitted without license from IHS --`,,```,,,,````-`-`,,`,,`,`,,`---//^:^^#^~^^"~~::"^#$~@@""#:$@:@"^$*~*"~~#^^$^@^~"#~~:\\。
高温合金AMS-5663M-N07718
SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright © 2004 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying,recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER:Tel: 877-606-7323 (inside USA and Canada)T el: 724-776-4970 (outside USA)Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18FeConsumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated(Composition similar to UNS N07718)1.SCOPE:1.1Form:This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.1.2Application:These products have been used typically for parts requiring high resistance to creep andstress-rupture up to 1300 °F (704 °C) and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications.2.APPLICABLE DOCUMENTS:The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply.2.1 SAE Publications:Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or .AMS 2261Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS 2269Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt AlloysAEROSPACE MATERIALSPECIFICATIONAMS 5663MIssued SEP 1965RevisedJUL 2004Superseding AMS 5663L2.1 (Continued):AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy ForgingsAMS 2750 PyrometryAMS 2806Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAMS 2808Identification, ForgingsAMS 7490Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels,Austenitic-Type Iron, Nickel, or Cobalt Alloys or Precipitation-Hardenable Alloys ARP1313 Determination of Trace Elements in High-Temperature Alloys2.2 ASTM Publications:Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or .ASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 10 Brinell Hardness of Metallic MaterialsASTM E 21 Elevated Temperature Tension Tests of Metallic MaterialsASTM E 103Rapid Indentation Hardness Testing of Metallic MaterialsASTM E 112Determining Average Grain SizeASTM E 139Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E 292Conducting Time-for-Rupture Notch Tension Tests of MaterialsASTM E 354Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys3.TECHNICAL REQUIREMENTS:3.1Composition:Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, by the methods of ARP1313 for lead, bismuth, and selenium, or by other analytical methods acceptable to purchaser.3.1.1Determination not required for routine analysis.3.1.2Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269.3.2Melting Practice:Alloy shall be multiple melted using consumable electrode practice in the remelt cycle or shall be induction melted under vacuum. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.3.3Condition:The product shall be supplied in the following condition.3.3.1Bars: Hot or cold finished, solution and precipitation heat treated, and descaled except as specified in 3.3.1.1 and 3.3.1.2.TABLE 1 - CompositionElementmin maxCarbon -- 0.08Manganese -- 0.35Silicon-- 0.35Phosphorus -- 0.015Sulfur-- 0.015Chromium 17.0021.00Nickel50.0055.00Molybdenum2.803.30Columbium (Niobium)4.755.50Titanium 0.65 1.15Aluminum 0.200.80Cobalt-- 1.00Tantalum (3.1.1)-- 0.05Boron -- 0.006Copper -- 0.30Lead -- 0.0005 (5 ppm)Bismuth -- 0.00003 (0.3 ppm)Selenium -- 0.0003 (3 ppm)Ironremainder--`,,,```,,,,,`,,`,`,,`,,````-`-`,,`,,`,`,,`---3.3.1.1Hot finished round bars shall be ground or turned; all other hot finished bars shall be as hotfinished.3.3.1.2Cold finished round bars shall be ground or as cold finished; all other cold finished bars shall beas cold finished.3.3.2Forgings and Flash Welded Rings: Solution and precipitation heat treated and descaled.3.3.2.1Flash welded rings shall not be supplied unless specified or permitted on purchaser's partdrawing. When supplied, rings shall be manufactured in accordance with AMS 7490.3.3.3Stock for Forging or Flash Welded Rings: As ordered by the forging or flash welded ringmanufacturer.3.4Heat Treatment:Bars, forgings, and flash welded rings shall be solution and precipitation heat treated in accordance with 3.4.1 and 3.4.2; pyrometry shall be in accordance with AMS 2750.3.4.1Solution Heat Treatment: Heat to a temperature within the range 1725 to 1850 °F (941 to 1010 °C),hold at the selected temperature within ±25 °F (±14 °C) for a time commensurate withcross-sectional thickness, and cool at a rate equivalent to an air cool or faster.3.4.1.1If forgings are not to be machined all over, heat treatment shall be performed in a suitableprotective atmosphere or, when permitted by purchaser, a suitable protective coating may beapplied to the forgings in lieu of using a protective atmosphere.3.4.2Precipitation Heat Treatment: Heat to a temperature within the range 1325 to 1400 °F(718 to 760 °C), hold at the selected temperature within ±15 °F (±8 °C) for approximately 8 hours, cool at 100 °F ± 15 (56 °C ± 8) degrees per hour to a temperature within the range 1150 to 1200 °F (621 to 649 °C), hold at the selected temperature within ±15 °F (±8 °C) for approximately 8 hours, and air cool. Instead of the 100 °F (56 °C) degrees per hour cooling rate to 1150 to 1200 °F(621 to 649 °C), the product may be furnace cooled at any rate provided the time at1150 to 1200 °F (621 to 649 °C) is adjusted to give a total precipitation heat treatment time ofapproximately 18 hours.3.5Properties:The product shall conform to the following requirements:3.5.1Bars, Forgings, and Flash Welded Rings:3.5.1.1Average Grain Size: Shall be as follows, determined in accordance with ASTM E 112. In case ofdisagreement, the intercept (Heyn) procedure shall be used.--` , , , ` ` ` , , , , , ` , , ` , ` , , ` , , ` ` ` ` -` -` , , ` , , ` , ` , , ` ---3.5.1.1.1Bars and flash welded rings under 9 square inches (58 cm2) in cross-sectional area shallexhibit an average grain size of ASTM No. 5 or finer. Due to the presence of nonrecrystallizedgrains, up to 20% of the cross section of the product may have an average grain size of ASTMNo. 3 to 5, determined by the intercept method of ASTM E 112.3.5.1.1.2Bars and flash welded rings 9 to 50 square inches (58 to 323 cm2), inclusive, in cross-sectionalarea and all forgings shall exhibit an average grain size of ASTM No. 4 or finer. Due to thepresence of nonrecrystallized grains, up to 20% of the cross section of the product may havean average grain size of ASTM No. 2 to 4, determined by the intercept method of ASTM E 112.3.5.1.2Microstructure: Product shall be free of Laves phase. Banding of acicular phase and amount ofacicular phase shall conform to standards acceptable to purchaser.3.5.1.3Tensile Properties: Product, 5.0 inches (127 mm) and under in least nominal cross-sectionaldimension, shall have the following properties:3.5.1.3.1At Room Temperature: Shall be as shown in Table 2, determined in accordance withASTM E 8 or ASTM E 8M.TABLE 2A - Minimum Room Temperature Tensile Properties, Inch/Pound UnitsSpecimen OrientationTensileStrengthksiYield Strengthat 0.2% OffsetksiElongationin 4D%Reduction ofArea%Longitudinal1851501215 Long-Transverse(Forgings)1801501012Transverse(Bars)180150 6 8 TABLE 2B - Minimum Room Temperature Tensile Properties, SI UnitsSpecimen OrientationTensileStrengthMPaYield Strengthat 0.2% OffsetMPaElongationin 4D%Reduction ofArea%Longitudinal127610341215 Long-Transverse(Forgings)124110341012Transverse(Bars)12411034 6 83.5.1.3.2At 1200 °F (649 °C): Shall be as shown in Table 3, determined in accordance withASTM E 21 on specimens heated to 1200 °F ± 5 (649 °C ± 3), held at heat for not less than 20 minutes before testing, and tested at 1200 °F ± 5 (649 °C ± 3).3.5.1.3.3Longitudinal requirements of 3.5.1.3.1 and 3.5.1.3.2 apply to specimens taken with the axis approximately parallel to the grain flow, to specimens taken in the radial direction and in the tangential direction at the rim of disc forgings, and to specimens taken in the circumferential direction from flash welded rings. All other specimens shall be considered to be in the transverse direction.3.5.1.3.4Transverse tensile properties apply only to product from which a test specimen not less than 2.50 inches (63.5 mm) long can be taken.3.5.1.3.5Specific locations of specimens from forgings and flash welded rings shall be as agreed upon by purchaser and vendor.TABLE 3A - Minimum Tensile Properties at 1200 °F, Inch/Pound Units Specimen Orientation Tensile Strength ksi Yield Strength at 0.2% OffsetksiElongation in 4D %Reduction ofArea %Longitudinal 1451251215Long-Transverse (Forgings)1401251012Transverse (Bars)140125 6 8TABLE 3B - Minimum Tensile Properties at 649 °C, SI UnitsSpecimen Orientation Tensile Strength MPa Yield Strength at 0.2% OffsetMPaElongation in 4D %Reduction ofArea %Longitudinal 10008621215Long-Transverse (Forgings)9658621012Transverse (Bars)965862 6 8--`,,,```,,,,,`,,`,`,,`,,````-`-`,,`,,`,`,,`---3.5.1.4Hardness: Shall be not lower than 331 HB, or equivalent (See 8.2), determined in accordancewith ASTM E 10 or ASTM E 103. Product shall not be rejected on the basis of hardness if thetensile property requirements of 3.5.1.3.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similarnonconforming hardness.3.5.1.5Stress-Rupture Properties at 1200 °F (649 °C): Shall be as follows; testing of notched specimensand of combination smooth-and-notched specimens shall be performed in accordance withASTM E 292 and of smooth specimens in accordance with ASTM E 139:3.5.1.5.1 A standard cylindrical combination smooth-and-notched specimen conforming to ASTM E 292,maintained at 1200 °F ± 3 (649 °C ± 2) while a load sufficient to produce an initial axial stress of100 ksi (689 MPa) or higher is applied continuously, shall not rupture in less than 23 hours. Thetest shall be continued to rupture without change of load. Rupture shall occur in the smoothsection and elongation of this section after rupture, measured at room temperature, shall be notless than 4% in 4D for product 5.0 inches (127 mm) and under in nominal diameter or leastdistance between parallel sides.3.5.1.5.2As an alternate procedure, separate smooth and notched specimens, machined from adjacentsections of the same piece, with gage sections conforming to the respective dimensions shownin ASTM E 292 may be tested individually under the conditions of 3.5.1.5.1. The smoothspecimen shall not rupture in less than 23 hours and elongation after rupture, measured atroom temperature, shall be as specified in 3.5.1.5.1. The notched specimen shall not rupture inless time than the companion smooth specimen but need not be tested to rupture.3.5.1.5.3The tests of 3.5.1.5.1 and 3.5.1.5.2 may be conducted using incremental loading. In such case,the load required to produce an initial axial stress of 100 ksi (689 MPa) or higher shall be usedto rupture or for 23 hours, whichever occurs first. After the 23 hours and at intervals of8 hours minimum, thereafter, the stress shall be increased in increments of 5.0 ksi (34.5 MPa).Time to rupture, rupture location, and elongation requirements shall be as specified in3.5.1.5.1.3.5.2Forging Stock: When a sample of stock is forged to a test coupon and solution and precipitationheat treated as in 3.4, specimens taken from the heat treated coupon shall conform to therequirements of 3.5.1.1, 3.5.1.2, 3.5.1.3, 3.5.1.4, and 3.5.1.5. If specimens taken from the stock after solution and precipitation heat treatment as in 3.4 conform to the requirements of 3.5.1.1,3.5.1.2, 3.5.1.3, 3.5.1.4, and 3.5.1.5, the tests shall be accepted as equivalent to tests of a forgedcoupon.3.5.3Stock for Flash Welded Rings: Specimens taken from the stock after heat treatment as in 3.4 shallconform to the requirements of 3.5.1.1, 3.5.1.2, 3.5.1.3, 3.5.1.4, and 3.5.1.5.3.6Quality:The product, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections detrimental to usage of the product.--` , , , ` ` ` , , , , , ` , , ` , ` , , ` , , ` ` ` ` -` -` , , ` , , ` , ` , , ` ---3.6.1Grain flow of die forgings, except in areas which contain flash-line end grain, shall follow thegeneral contour of the forging showing no evidence of reentrant grain flow.3.7Tolerances:Bars shall conform to all applicable requirements of AMS 2261.4.QUALITY ASSURANCE PROVISIONS:4.1Responsibility for Inspection:The vendor of the product shall supply all samples for vendor's tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform anyconfirmatory testing deemed necessary to ensure that the product conforms to specifiedrequirements.4.2Classification of Tests:4.2.1Acceptance Tests: The following requirements are acceptance tests and shall be performed oneach heat or lot as applicable:4.2.1.1Composition (3.1) of each heat.4.2.1.2Average grain size (3.5.1.1), tensile properties (3.5.1.3), hardness (3.5.1.4), and stress-ruptureproperties (3.5.1.5) of each lot of bars, forgings, and flash welded rings.4.2.1.3Microstructure (3.5.1.2) of each lot.4.2.1.4Tolerances (3.7) of bars.4.2.2Periodic Tests: Tests of forging stock (3.5.2) and of stock for flash welded rings (3.5.3) to --`,,,```,,,,,`,,`,`,,`,,````-`-`,,`,,`,`,,`---demonstrate ability to develop required properties and of grain flow of die forgings (3.6.1) areperiodic tests and shall be performed at a frequency selected by the vendor unless frequency of testing is specified by purchaser.4.3Sampling and Testing:Shall be as follows:4.3.1Bars, Flash Welded Rings, and Stock for Forging or Flash Welded Rings: In accordance withAMS 2371.4.3.2Forgings: In accordance with AMS 2374.4.4Reports:4.4.1The vendor of bars, forgings, and flash welded rings shall furnish with each shipment a reportshowing the results of tests and relevant information:4.4.1.1For each heat:Composition4.4.1.2For each lot:Average grain sizeMicrostructure resultsRoom temperature tensile properties1200 °F (649 °C) tensile propertiesHardnessStress-rupture properties.4.4.1.3 A statement that the product conforms to the other technical requirements.4.4.1.4Purchase order numberHeat and lot numbersAMS 5663MSizeQuantity.4.4.1.5If forgings are supplied, the size and melt source of stock used to make the forgings.4.4.2The vendor of stock for forging or flash welded rings shall furnish with each shipment a reportshowing the results of tests for the composition of each heat. This report shall include the purchase order number, heat and lot number, AMS 5663M, size, and quantity.4.5Resampling and Retesting:Shall be as follows:4.5.1Bars, Flash Welded Rings, and Stock for Forging or Flash Welded Rings: In accordance withAMS 2371.4.5.2Forgings: In accordance with AMS 2374.5.PREPARATION FOR DELIVERY:5.1Sizes:Except when exact lengths or multiples of exact lengths are ordered, straight bars will be acceptable in mill lengths of 6 to 24 feet (1.8 to 7.3 m) but not more than 25% of any shipment shall be supplied in lengths of 6 to 9 feet (1.8 to 2.7 m) except that for bars weighing over 25 pounds per foot(37 kg/m), short lengths down to 2 feet (610 mm) may be supplied.5.2Identification:Shall be as follows:5.2.1Bars: In accordance with AMS 2806.5.2.2Forgings: In accordance with AMS 2808.5.2.3Flash Welded Rings and Stock for Forging or Flash Welded Rings: As agreed upon by purchaserand vendor.5.3Packaging:The product shall be prepared for shipment in accordance with commercial practice and incompliance with applicable rules and regulations pertaining to the handling, packaging, andtransportation of the product to ensure carrier acceptance and safe delivery.6.ACKNOWLEDGMENT:A vendor shall mention this specification number and its revision letter in all quotations and whenacknowledging purchase orders.7.REJECTIONS:Product not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection.8.NOTES:8.1 A change bar (|) located in the left margin is for the convenience of the user in locating areas wheretechnical revisions, not editorial changes, have been made to the previous issue of a specification.An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revisions. Change bars and (R) are not used in original publications, nor inspecifications that contain editorial changes only.8.2Hardness conversion tables for metals are presented in ASTM E 140.8.3Terms used in AMS are clarified in ARP1917.--` , , , ` ` ` , , , , , ` , , ` , ` , , ` , , ` ` ` ` -` -` , , ` , , ` , ` , , ` ---AMS 5663M SAE AMS 5663M- 11 -8.4Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary;dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.8.5Purchase documents should specify not less than the following:AMS 5663MForm and size or part number of product desiredQuantity of product desiredIf applicable, specific location of tensile specimens from forgings and flash welded rings (See 3.5.1.3.5).8.6Key Words:UNS N07718, solution heat treated, precipitation heat treated, bars, forgings, rings, stress-rupture, grain size, microstructure, 1200 °F tensilePREPARED UNDER THE JURISDICTION OF AMS COMMITTEE “F”Copyright SAE InternationalProvided by IHS under license with SAELicensee=Parker Hannifin - Categories/5936628103 Not for Resale, 08/31/2006 16:59:08 MDT No reproduction or networking permitted without license from IHS --`,,,```,,,,,`,,`,`,,`,,````-`-`,,`,,`,`,,`---。
AMS5665镍铬合金
AMS5665镍铬合金
ASTM B163 –无缝镍和镍合金冷凝器和热交换器管的标准规范
ASTM B166 –镍铬铁合金标准规范（UNS N06600，N06601，N06603，N06690，N06693，N06025，N06045和N06696）*和镍铬钴钴钼合金（UNS N06617）棒，棒和棒线
ASTM B167 –镍铬铁合金（UNS N06600，N06601，N06603，N06690，N06693，N06025，N06045和N06696）的标准规范*和镍铬钴钴钼合金（UNS N06617）无缝管
ASTM B168 –镍铬铁合金（UNS N06600，N06601，N06603，N06690，N06693，N06025，N06045和N06696）和镍铬钴钴钼合金（UNS N06617）板，片和带的标准规范
ASTM B366 –工厂制造的锻造镍和镍合金配件的标准规范
ASTM B516 –镍铬铁合金焊接标准规范（UNS N06600，UNS N06603，UNS N06025和UNS N06045管
ASTM B517 –镍铬铁合金焊接标准规格（UNS N06600，UNS N06603，UNS N06025和UNS N06045）
ASTM B564 –镍合金锻件的标准规范
ASTM B751 –镍和镍合金焊接管通用要求的标准规范
MIL-R-5031 –棒和钢丝，焊接，耐腐蚀和耐热合金
MIL-T-23227 –管和管，镍铬铁合金（UNS N06600）
MIL-N-23228 –镍铬铁合金板，片和带
MIL-N-23229 –镍铬铁合金棒料和锻件
ASME SB-163，SB-166 – SB-168，SB-564
纳斯MR-01-75
QQ-W-390。
镍基合金材料标准
镍基合金材料标准镍基合金是一类重要的高温合金材料，具有良好的耐高温、耐腐蚀、高强度和良好的加工性能等优点，被广泛应用于航空航天、石油化工、核能、船舶制造等领域。
为了规范镍基合金材料的生产、加工和使用，制定了一系列的相关标准。
下面将对镍基合金材料的标准进行详细介绍。
一、镍基合金材料的分类标准根据合金成分和性能特点的不同，镍基合金材料可以分为多种不同的类型。
目前国内外普遍采用的是美国标准和欧洲标准，其中美国标准主要由ASTM（美国材料与试验协会）负责制定，欧洲标准主要由ISO（国际标准化组织）负责制定。
1. 美国标准在美国，镍基合金材料通常按照ASTM标准进行分类。
ASTM标准共包括了近百种针对不同合金成分和性能特点的镍基合金材料标准，例如ASTM B166/B166M-09 标准规定了无缝镍及镍合金管，ASTM B574-10a 标准规定了镍铬钼钨合金棒料等。
这些标准主要规定了合金材料的化学成分、力学性能、加工工艺等方面的要求，为生产厂家提供了明确的生产和质量控制依据。
2. 欧洲标准在欧洲地区，镍基合金材料的标准主要由ISO负责制定。
ISO标准包括了许多与合金成分、性能、加工等相关的技术规范，具有较高的权威性和通用性。
比如ISO5832-12:2013为医疗器械用高温合金规定了特殊要求等。
这些标准被广泛应用于工程设计、生产制造、检测认证等方面，对保障镍基合金材料的质量和安全起到了至关重要的作用。
二、镍基合金材料的生产和检测标准1. 生产标准除了对镍基合金材料的化学成分和性能进行规范外，生产标准也是镍基合金行业中非常重要的一部分。
生产标准主要涉及原料选用、熔炼制备、热处理工艺、加工方法等方面的要求。
还包括了对生产设备、环境、技术人员的要求，以及对产品质量控制和追溯体系的要求。
这些标准能够有效指导生产厂家合理开展生产活动，确保产品质量和生产安全。
2. 检测标准镍基合金材料的质量检测是确保产品质量和安全的重要环节。
SAE标准目录
ETA-UTP001 Revision 0(SAE J1263)[P19].pdfETA-UTP001-Effective March 23,2001 Implementation of SAE J1263-1996.pdfNASA-SAE-88-1448 LDV Surveys Over Fighter Model at Moderate High Angles of Attack[P27].pdf SAE- Automotive Chassis Engineering Principles (SECOND EDITION)[P454].pdfSAE- Automotive Chassis-Engineering Principles [SECOND EDITION][P456].pdfSAE- Automotive Physical Layer SAE-J1708 DS36277.pdfSAE- Structural Steel Designer's Handbook (Brockenbrough & Merritt)(3Rd Edition)[P1201].pdf SAE-174M-MAY1998 TORQUE-TENSION TEST PROCEDURESTEEL THREADED FASTENERS,METRIC SERIES.pdfSAE-2006 Formula SAE-Chassis Design(Queen's University)[P18].pdfSAE-720709-1972 Design&Development of a High horsepower torque sensing variable speed drive.pdfSAE-AIR1228-2001 Standard Impulse Machine Equipment&Operation[P6].pdfSAE-AIR1377A-2004 Fire Test Equipment for Flexible Hose&Tube Assemblies[P22].pdfSAE-AIR3260-2006 Identification of Standard Utility Parts - Bolts&Nuts[P4].pdfSAE-AIR4002-1994 8000 psi Hydraulic Systems Experience&Test Results.pdfSAE-AIR4069A-1998 Sealing of Integral Fuel Tanks [P94].pdfSAE-AIR4069A-1998 Sealing of Integral Fuel Tanks[P95].pdfSAE-AIR4176-1995(R2005) Cost Versus Benefits of Engine Monitoring Systems.pdfSAE-AIR5120-2006 Engine Monitoring System Reliability&Validity[P27].pdfSAE-AIR797E-2001 Hose Characteristics&Selection Chart[P15].pdfSAE-AMS1376B-1992 R1998 Remover,Epoxy Paint Acid-Type,Thickened.pdfSAE-AMS1379A-1996 COMPOUND,ALKALINE RUST REMOVER Aircraft Turbine Engine Components[P7].pdfSAE-AMS1380A-1992 SCALE CONDITIONER,ALKALINE Aircraft Turbine Engine Components[P6].pdfSAE-AMS1382A-1991 OXIDE REMOVER COMPOUND,ACIDIC Aircraft Turbine Engine Components[P6].pdfSAE-AMS1383A-1999 Oxide Conditioner,Alkaline Permanganate Aircraft Turbine Engine Components.pdfSAE-AMS1384A-1991 ACID,INHIBITED PHOSPHORIC Aircraft Turbine Engine Components Room Temperature Application[P6].pdfSAE-AMS1385A-2004 Compound,Hot Carbon&Paint Remover Aircraft Turbine Engine Components.pdfSAE-AMS1386A-2004 Compound,Silicone Rubber Remover Aircraft Turbine Engine Components Room Temperature Application.pdfSAE-AMS1387A-2004 Remover,Anti-Galling Compound Aircraft Turbine Engine Components Room Temperature Application.pdfSAE-AMS1424G-2006 (R) Deicing_Anti-Icing Fluid,Aircraft SAE-Type I.pdfSAE-AMS1424H-2007 Deicing_Anti-Icing Fluid,Aircraft,SAE-Type I[P15].pdfSAE-AMS1426C-1993 FLUID,DEICINGANTI-ICING,RUNWAYS&TAXIWAYS Glycol Base.pdf SAE-AMS1428E-2006 Fluid,Aircraft DeicingAnti-Icing,Non-Newtonian (Pseudoplastic),SAE-Types II,III,&IV.pdfSAE-AMS1431B-1998 Compound,Solid Runway&Taxiway Deicing_Anti-Icing.pdfSAE-AMS1435A-1999 Fluid,Generic,Deicing_Anti-Icing Runways&Taxiways.pdfSAE-AMS1453-2004 Disinfectant Cleaner for Aircraft Interior General Purpose Liquid .pdfSAE-AMS1476B-2004 Deodorant,Aircraft Toilet.pdfSAE-AMS1526B-2000 Cleaner for Aircraft Exterior Surfaces Water-Miscible,Pressure-Spraying Type.pdfSAE-AMS1534B-2004 Cleaner,Aircraft Glass Window.pdfSAE-AMS1535C-2002 Cleaner,Transparent Plastic.pdfSAE-AMS1537B-2001 Cleaner,Alkaline Hot-Tank Type.pdfSAE-AMS1538A-1996 DEOXIDER,ACIDIC,FOR MAGNESIUM ALLOYS.pdfSAE-AMS1547-1996 Cleaner,Anodic,Electrolytic,Alkaline For Steel,Tank Type .pdfSAE-AMS1595A-1998 Qualification of Aircraft,Missile&Aerospace Fusion Welders.pdfSAE-AMS1625B-1989 DESMUTTER,ALUMINUM,POWDERED.pdfSAE-AMS1626B-1989 DESMUTTER,ALUMINUM Liquid.pdfSAE-AMS1631C-2005 Cleaner,Carpet Water Extraction Type.pdfSAE-AMS1640B-1988 CORROSION REMOVING COMPOUND For Aircraft Surfaces.pdfSAE-AMS2154-2005 Inspection,Ultrasonic,Wrought Metals,Process For.pdfSAE-AMS2154-2005 Inspection,Ultrasonic,Wrought Metals,Process For[P41].pdfSAE-AMS2175-2003 Castings,Classification&Inspection of.pdfSAE-AMS2241P-2005 Tolerances,Corrosion&Heat-Resistant Steel,Iron Alloy,Titanium,&Titanium Alloy Bars&Wire.pdfSAE-AMS2242F-2006 Tolerances Corrosion&Heat Resistant Steel,Iron Alloy,Titanium,&Titanium Alloy Sheet,Strip,&Plate.pdfSAE-AMS2243H-2006 Tolerances Corrosion&Heat-Resistant Steel Tubing.pdfSAE-AMS2244C-2003 Tolerances (R) Titanium&Titanium Alloy Tubing.pdfSAE-AMS2249F-2005 Chemical Check Analysis Limits Titanium&Titanium Alloys.pdfSAE-AMS2249F-2005 Chemical Check Analysis Limits Titanium&Titanium Alloys[1].pdfSAE-AMS2251G-1998 Tolerances Low-Alloy Steel Bars.pdfSAE-AMS2251H-2006 Tolerances Low-Alloy Steel Bars.pdfSAE-AMS2252D-2006 Tolerances Low-Alloy Steel Sheet,Strip,&Plate.pdfSAE-AMS2269F-2006 Chemical Check Analysis Limits Nickel,Nickel Alloys,and Cobalt Alloys.pdf SAE-AMS2372D 碳钢和低合金钢取样规范[中文版].pdfSAE-AMS2372D-JAN2002 Quality Assurance Sampling&Testing Carbon&Low-Alloy Steel Forgings[P6].pdfSAE-AMS2375D-2007 Control of Forgings Requiring First Article Approval [P6].pdfSAE-AMS2406L-2007 Plating,Chromium Hard Deposit [p7].pdfSAE-AMS2411F-2007 Plating,Silver for High Temperature Applications [P8].pdfSAE-AMS2412H-2007 Plating,Silver Copper Strike,Low Bake[P7].pdfSAE-AMS2417G-2004 Plating,Zinc-Nickel Alloy.pdfSAE-AMS2422E-2007 Plating,Gold[P9].pdfSAE-AMS2435G-2007 Coating,Tungsten Carbide-Cobalt Coating,Detonation Process [P8].pdfSAE-AMS2448-2004 Application of Tungsten Carbide Coatings on Ultra High Strength Steels High Velocity Oxygen Fuel Process[P13].pdfSAE-AMS2448-2004 Application of Tungsten Carbide Coatings on Ultra High Strength Steels High Velocity Oxygen Fuel Process.pdfSAE-AMS2469G-2004 Hard Anodic Coating Treatment of Aluminum&Aluminum Alloys Processing&Performance Requirements.[P8].pdfSAE-AMS2470M-2007 Anodic Treatment of Aluminum Alloys Chromic Acid Process[P8].pdfSAE-AMS2482C-2006 Hard Coating Treatment of Aluminum Alloys Teflon-Impregnated or Codeposited.pdfSAE-AMS2482C-2006 Hard Coating Treatment of Aluminum Alloys Teflon-Impregnated or Codeposited[P7].pdfSAE-AMS2546-2004 Reaffirmed 2010-05 Laser Peening.pdfSAE-AMS2633C-2007 Ultrasonic Inspection Centrifugally-Cast,Corrosion-Resistant Steel Tubular Cylinders[P13].pdfSAE-AMS2643D-2007 Structural Examination of Titanium Alloys Chemical Etch Inspection Procedure [P5].pdfSAE-AMS2647C-2009 Fluorescent Penetrant Inspection Aircraft&Engine Component Maintenance.pdfSAE-AMS2649C-2008 Etch Inspection of High Strength Steel Parts.pdfSAE-AMS2753B-1991 Liquid Salt Bath Ferritic Nitrocarburizing Non-Cyanide Bath[P8].pdfSAE-AMS2757-B-2004 气体氮碳共渗.pdfSAE-AMS2759_11-2005 Stress Relief of Steel Parts[P5].pdfSAE-AMS2759_2C-2000 低合金钢零件的热处理最小拉伸强度大于等于220KSI[中文版][P13].pdfSAE-AMS2759_3C-2000 沉淀硬化不锈钢和马氏体时效钢的热处理[中文版][P16].pdfSAE-AMS2759_3D-2005 Heat Treatment Precipitation-Hardening Corrosion-Resistant&Maraging Steel Parts[P16].pdfSAE-AMS2759_3D-2005 Heat Treatment Precipitation-Hardening Corrosion-Resistant&Maraging Steel Parts[P16][1].pdfSAE-AMS2759-11-1992 Ion Nitriding.pdfSAE-AMS2759-11-2005 Stress Relief of Steel Parts.pdfSAE-AMS27591-12A-2007 Gaseous Nitrocarburizing,Automatically Controlled by Potentials.pdf SAE-AMS2759-12A 2007 Gaseous Nitrocarburizing,Automatically Controlled by Potentials.pdfSAE-AMS2759-1C-2000 最低抗拉强度低于220 ksi (1517 MPa)低合金碳钢零件的热处理.pdf SAE-AMS2759-2C-2000 Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1 51 7 MPa)&Higher.pdfSAE-AMS2759-2C-2000 中文版低合金钢零件的热处理最小拉伸强度大于等于220KSI(1517MPa).pdfSAE-AMS2759-3C-2000 中文版沉淀硬化不锈钢和马氏体时效钢的热处理.pdfSAE-AMS2759-3D-2005 Heat Treatment Precipitation-Hardening Corrosion-Resistant&Maraging Steel Parts.pdfSAE-AMS2759-4B-2001 Heat Treatment Austenitic Corrosion-Resistant Steel Parts.pdfSAE-AMS2759-5D-2004 Heat Treatment Martensitic Corrosion-Resistant Steel Parts.pdfSAE-AMS2759-6A-2002 Gas Nitriding&Heat Treatment of Low-Alloy Steel Parts.pdfSAE-AMS2759-7A-2006 Carburizing&Heat Treatment of Carburizing Grade Steel Parts.pdfSAE-AMS2759-9_8-1992 Ion Nitriding [P12].pdfSAE-AMS2759C-2000 Heat Treatment of Steel Parts General Requirements[P15].pdfSAE-AMS2770H-2006 Heat Treatment of Wrought Aluminum Alloy Parts.pdfSAE-AMS2771C-2004 Heat Treatment of Aluminum Alloy Castings.pdfSAE-AMS2772C-2002 Heat Treatment of Aluminum Alloy Raw Materials.pdfSAE-AMS2772E-2008 Heat Treatment of Aluminum Alloy Raw Materials.pdfSAE-AMS2809-1986 R2002 Identification Titanium&Titanium Alloy Wrought Products.pdfSAE-AMS2809-2002 Identification Titanium&Titanium Alloy Wrought Products.pdfSAE-AMS2814F-2001 优质焊丝包的包装和标识.pdfSAE-AMS2814F-2001 优质焊丝包的包装和标识[P8].pdfSAE-AMS3021D-2007 Fluid,Reference for Testing Di-Ester (Polyol) Resistant Material [P4].pdfSAE-AMS3302G-1990 Silicone Rubber,General Purpose,50 Durometer.pdfSAE-AMS3650C-1991 Rods,Sheets,&Molded Shapes,Polychlorotrifluoroethylene (PCTFE),Unplasticized.pdfSAE-AMS3901C-1998 Organic Fiber (Para-Aramid),Yarn&Roving,High Modulus[P13].pdfSAE-AMS4045J-2007 Aluminum Alloy Sheet&Plate 5.6Zn-2.5Mg-1.6Cu-0.23Cr 7075 (-T6 Sheet,-T651 Plate)[P5].pdfSAE-AMS4100D-2007 Aluminum Alloy,Alclad,Sheet 5.7Zn-2.2Mg-1.6Cu-0.22Cr (Alclad 7475-T761)[P6].pdfSAE-AMS4108F-2003 Aluminum Alloy,Hand Forgings 6.2Zn-2.3Cu-2.2Mg-0.12Zr (7050-T7452)Solution Heat Treated,Compression Stress-Relieved,and Overaged.pdfSAE-AMS4111D-2007 Aluminum Alloy Forgings 7.7Zn-2.5Mg-1.5Cu-0.16Cr (7049-T73)[P8].pdf SAE-AMS4143D-2001 Aluminum Alloy Forgings&Rolled or Forged Rings 6.3Cu-0.30Mn-0.18Zr-0.10V-0.06Ti (2219-T6) Solution&Precipitation Heat Treated.pdfSAE-AMS4147D-2007 Aluminum Alloy Forgings 5.6Zn-2.5Mg-1.6Cu-0.23Cr(7075-T7352) Solution Heat Treated,Stress Relieved by Compression,&Overaged[P7].pdfSAE-AMS4150L-2003(R2008) Aluminum Alloy,Extrusions&Rings 1.0Mg-0.60Si-0.28Cu-0.20Cr-(6061-T6) Solution&Precipitation Heat Treated.pdfSAE-AMS4152M-2007 Aluminum Alloy,Extrusions 4.4Cu 1.5Mg 0.60Mn Solution Heat Treated[P5].pdfSAE-AMS4157D-2007 Aluminum Alloy Extrusions 7.7Zn-2.4Mg-1.6Cu-0.16Cr (7049-T73511)[P5].pdfSAE-AMS4162D-2003 Aluminum Alloy,Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T8511) Solution Treated,Stress Relief Stretched,Straightened,&Precipitation Heat Treated.pdf SAE-AMS4169K-2003 Aluminum Alloy,Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6511)&Precipitation Heat Treated.pdfSAE-AMS4173E-2003 Aluminum Alloy,Extrusions 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T6511) Solution Heat Treated Stress.pdfSAE-AMS4206A-2006 Aluminum Alloy,Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated,Stress Relieved,&Overaged.pdfSAE-AMS4218H-2001 Aluminum Alloy Castings 7.0Si 0.35Mg (A356.0-T6P) (Formerly T61P Temper) Solution&Precipitation Heat Treated.pdfSAE-AMS4270B-2007 Aluminum Alloy,Alclad Flat Sheet 4.1Cu-1.4Mg-0.45Mn (Alclad 2424-T3) [P7].pdfSAE-AMS4279B-2006 Aluminum Alloy,Alclad Sheet 4.4Cu 1.5Mg 0.60Mn (2024-T4 Flat Sheet) Solution Heat Treated,High Formability.pdfSAE-AMS4324-2002(R2007) 固溶热处理的、消除应力的和过老化的(7055-T74511)含8.0Zn-2.3Cu-2.0Mg-0.16Zr挤压的铝合金杆材、棒材和型材.pdfSAE-AMS4329A-2006 Aluminum Alloy,Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated,Stress-Relieved,&Ove[P6].pdfSAE-AMS4337A-2006 Aluminum Alloy,Extruded Profiles (7055-T77511) 8.0Zn 2.3Cu 2.0Mg 0.16Zr Solution Heat Treated,Stress Relieved,&Overaged.pdfSAE-AMS4342E-2007 Aluminum Alloy,Extrusions 6.2Zn 2.3Cu 2.2Mg 0.12Zr (7050-T74511) Solution Heat Treated,Stress Relieved,Straightened,&Overaged.pdfSAE-AMS4484K-2007 Magnesium Alloy Castings,Permanent Mold 9.0Al-2.0Zn (AZ92A-T6) [P7].pdfSAE-AMS4500J-2007 Copper,Sheet,Strip,and Plate Soft Annealed [P4].pdfSAE-AMS4640-2005 ALUMINUM BRONZE BARS. RODS. SHAPES. TUBES.&FORGINGS 81.5 CU- 10.A1 - 4.8NI - 3.0FE DRAWN&STRESS RELIEVED (HR50) OR TEMPER ANNEALED (TQ50[P8 OCR].pdfSAE-AMS4775H-2005 Nickel Alloy,Brazing Filler Metal 73Ni - 0.75C - 4.5Si - 14Cr - 3.1B - 4.5Fe 1790 to 1970 °F (977 to 1077 °C) Solidus-Liquidus Range.pdfSAE-AMS4805E-2007 Bearings,Sintered Metal Powder 89Cu-10Sn Oil Impregnated [P6].pdfSAE-AMS4900M-2006 AEROSPACE MATERIAL SPECIFICA TION Titanium Sheet,Strip,&Plate Commercially Pure Annealed,55 ksi (379 MPa) [P6].pdfSAE-AMS4911K-2007 Titanium Alloy,Sheet,Strip,and Plate 6AI-4V Annealed [P7].pdfSAE-AMS4911L-2007 Titanium Alloy,Sheet,Strip,and Plate 6AI-4V Annealed [P7].pdfSAE-AMS4918L-2006 Titanium Alloy,Sheet,Strip,&Plate6AI - 6V - 2Sn Annealed[P7].pdfSAE-AMS4921K-2006 [P8].pdfSAE-AMS4921L-2007 Titanium Bars,Wire,Forgings,and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength [P7].pdfSAE-AMS4928Q-2001 Titanium Alloy Bars,Wire,Forgings,Rings,&Drawn Shapes.pdfSAE-AMS4928R-2007 Titanium Alloy Bars,Wire,Forgings,Rings,&Drawn Shapes 6Al - 4V Annealed.pdfSAE-AMS4931B-2002 含6Al-4V超低填隙的、二次退火的、断裂韧度的钛合金棒材、锻件和环件.pdfSAE-AMS4931C-2007 Titanium Alloy bars,Forgings&Rings 6Al-4V Extra low interstitial(ELI) Duplex.pdfSAE-AMS4933D-2008 Titanium Alloy Extrusions and Flash Welded Rings 8Al-1Mo-1V Solution Heat Treated and Stabilized[P8].pdfSAE-AMS4942E-2006 Titanium Tubing,Seamless Annealed,40.0 ksi (275 MPa) Yield Strength.pdf SAE-AMS4943H-2008 Titanium Alloy.Hydraulic. Seamless Tubing 3.0Al-2.5V Annealed.pdfSAE-AMS4944G-2006 Titanium Alloy Tubing,Seamless,Hydraulic 3.0Al - 2.5V Cold Worked,Stress Relieved.pdfSAE-AMS4958C-2008 Titanium Alloy Bars and Rods 3Al-8V-6Cr-4Mo-4Zr Consumable Electrode Melted Solution Heat Treated and Centerless Ground[P6].pdfSAE-AMS4965J-2007 Titanium Alloy,Bars,Wire,Forgings,and Rings 6.0AI-4.0V Solution Heat Treated&Aged [P8].pdfSAE-AMS4971G-2007 Titanium Alloy,Bars,Wire,Forgings,and Rings 6Al-6V-2Sn Annealed,Heat Treatable[P8].pdfSAE-AMS4975J-2007 Titanium Alloy,Bars,Wire,andRings6.0Al-2.0Sn-4.0Zr-2.0Mo-0.08SiSolution&Precipitation Heat Treated[P7].pdfSAE-AMS4982D-2007 Titanium Alloy Wire 44.5 Cb [P6].pdfSAE-AMS5010K-2006 Steel Bars Free Machining Cold Drawn (SAE-1212 or SAE-1215) UNS G12120[P4].pdfSAE-AMS5046C-2007 Carbon Steel,Sheet,Strip,and Plate (SAE-1020&1025) Annealed[P5].pdfSAE-AMS5047F-2007 Steel,Sheet&Strip 0.08-0.13C,Aluminum Killed (SAE-1010) Deep Forming Grade [P4].pdfSAE-AMS5085G-2008 Steel Sheet. Strip.&Plate 0.47-0.55C (SAE-1050) Annealed.pdfSAE-AMS5349D-2007 Steel,Corrosion-Resistant,Investment Castings 13Cr Free Machining; Hardened&Tempered[P11].pdfSAE-AMS5352E-2007 Steel,Corrosion-Resistant,Investment Castings 17Cr-0.55Mo (0.95-1.20C) Annealed[P9].pdfSAE-AMS5353D-2007 Steel,Corrosion-Resistant,Investment Castings 16Cr-1.8Ni-0.08N ASCast [P10].pdfSAE-AMS5355H-2001 steel,corrosion resistant,investment casting[P14 OCR].pdfSAE-AMS5383E-2007 Nickel Alloy,Corrosion&Heat-Resistant,Investment Castings 52.5Ni-19Cr-3.0Mo-5.1Cb(Nb)-0.90Ti-0.60Al-18Fe[P11].pdfSAE-AMS5385G-1999 铸造状态的含62Co-27Cr-2.8Ni-5.5Mo耐腐蚀和耐热的钴合金熔模铸件.pdfSAE-AMS5398F-2006 Steel,Corrosion Resistant,Sand&Centrifugal Castings 16Cr 4.1Ni 0.22(Cb + Ta) 2.8Cu Solution Heat Treated[P9].pdfSAE-AMS5512L-2007 Steel,Corrosion&Heat-Resistant,Sheet,Strip,and Plate 18Cr-10.5Ni-0.80Cb (SAE-30347)Solution Heat Treated[P5].pdfSAE-AMS5516P-2007 Steel,Corrosion-Resistant,Sheet,Strip,and Plate 18Cr-9.0Ni (SAE-30302)Solution Heat Treated[P5].pdfSAE-AMS5542N-2007 Nickel Alloy,Corrosion&Heat-Resistant,Sheet,Strip,and Plate72Ni-15.5Cr-0.95Cb(Nb)-2.5Ti-0.70Al-7.0Fe[p6].pdfSAE-AMS5548P-2007 Steel,Corrosion&Heat-Resistant,Sheet&Strip 16.5Cr-4.5Ni-2.9Mo-0.10N 1850 to 1975 °F (1010 to 1079 °C) Annealed[P6].pdfSAE-AMS5561G-2007 Steel,Corrosion&Heat-Resistant,Welded&Drawn or Seamless&Drawn Tubing 9.0Mn-20Cr-6.5Ni-0.28N High-Pressure Hydraulic[P8].pdfSAE-AMS5569A-2001 Steel,Corrosion&Heat Resistant,Seamless&Welded Hydraulic Tubing 19Cr-9.5Ni-0.03C max Cold Drawn,1∕8 Hard Temper.pdfSAE-AMS5575N-2007 Steel,Corrosion&Heat-Resistant,Welded Tubing 18Cr-10.5Ni-0.70Cb(Nb) (SAE-30347)Solution Heat Treated[P6].pdfSAE-AMS5581D-2001 Nickel Alloy,Corrosion&Heat Resistant,Seamless or Welded Tubing 62Ni-21.5Cr-9.0Mo-3.7Cb Annealed.pdfSAE-AMS5589E-2007 Nickel Alloy,Corrosion&Heat-Resistant,Seamless Tubing 52.5Ni-19Cr-3.0Mo-5.1Cb (Nb)-0.90Ti-0.50Al-18Fe[P6].pdfSAE-AMS5596K-2007 Nickel Alloy,Corrosion&Heat-Resistant,Sheet,Strip,Foil&Plate 52.5Ni-19Cr-3.0Mo-5.1Cb (Nb)-0.90Ti-0.50Al-18Fe[P8].pdfSAE-AMS5599G-2007 Nickel Alloy,Corrosion&Heat-Resistant,Sheet,Strip,and Plate 62Ni-21.5Cr-9.0Mo-3.7 Cb (Nb)[P5].pdfSAE-AMS5612J-2007 Steel,Corrosion&Heat-Resistant,Bars,Wire,Forgings,Tubing,and Rings 12CrFerrite Controlled,Annealed[P7].pdfSAE-AMS5629E-2002 真空感应加真空自耗预热处理沉淀硬化型耐蚀13Cr-8.0Ni-2.2Mo-1.1Al钢棒、丝、锻件、环和模锻件.pdfSAE-AMS5630G-2000 Steel,Corrosion Resistant,Bars,Wire,and Forgings 17Cr-0.52Mo (0.95-1.20C) (SAE-51440C).pdfSAE-AMS5639H-2002(R2007) 管口连接用备份密封圈的六角螺母[P7].pdfSAE-AMS5643Q-2003 Steel,Corrosion-Resistant,Bars,Wire,Forgings,Tubing,and Rings 16Cr-4.0Ni-0.30Cb-4.0Cu Solution Heat Treated,Precipitation Hardenable.pdfSAE-AMS5659K-1998 Steel,Corrosion Resistant,Bars,Wire,Forgings,Rings,&Extrusions 15Cr - 4.5Ni - 0.30Cb - 3.5Cu Consumable Electrode Melted Solution Heat Treated,Precipitation Hardenable.pdf SAE-AMS5659L-2004 Steel,Corrosion-Resistant,Bars,Wire,Forgings,Rings,&Extrusions[P10].pdf SAE-AMS5662M-2004 镍基高温合金[P17].pdfSAE-AMS5668J-2007 Nickel Alloy,Corrosion&Heat-Resistant,Bars,Forgings,and Rings 72Ni-15.5Cr-7.0Fe-2.5Ti-1.0Cb (Nb)-0.70Al[P7].pdfSAE-AMS5678F-2002(R2007) Steel,Corrosion Resistant,Wire 17Cr-7.1Ni-1.1Al Cold Drawn,Precipitation-Hardenable-UNS S17700.pdfSAE-AMS5688L-2007 Steel,Corrosion Resistant,Wire 18Cr 9.0Ni (SAE-30302) Spring Temper.pdf SAE-AMS5698G-2003(R2007) Nickel Alloy,Corrosion&Heat-Resistant,Wire 72Ni-15.5Cr-0.95Cb-2.5Ti-0.70Al-7.0Fe No.1 Temper,Precipitation Hardenable-UNS N07750.pdf SAE-AMS5699G-2003(R2007) Nickel Alloy,Corrosion&Heat-Resistant,Wire 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe Spring Temper,Precipitation Hardenable.pdfSAE-AMS5713J-2007 Nickel Alloy,Corrosion&Heat-Resistant,Bars,Forgings,&Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted,Solution&Precipitation Heat Treated.pdfSAE-AMS5713J-2007 Nickel Alloy,Corrosion&Heat-Resistant,Bars,Forgings,and Rings 53Ni-19Cr-11Co-9.8Mo-3.2Ti-1.6Al-0.006B[P7].pdfSAE-AMS5732J-2006 Steel,Corrosion&Heat-Resistant,Bars,Wire,Forgings,Tubing,and Rings 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution&P.pdfSAE-AMS5759-2004 Cobalt Alloy,Corrosion&Heat-Resistant,Bars,Forgings,&Rings 52Co- 20Cr- 10Ni- 15W Solution Heat Treated.pdfSAE-AMS5772D-2004(R2009) Cobalt Alloy,Corrosion&Heat-Resistant,Bars,Forgings&Rings 40Co 22Cr 22Ni 14.5W 0.07La,Solution Heat Treated.pdfSAE-AMS5786E-2002 Nickel Alloy,corrosion&heat-resistant,welding wire 62.5Ni-5.0Cr-24.5Mo-5.5Fe.pdfSAE-AMS5796D-2000 Cobalt Alloy,Corrosion&Heat Resistant,Welding Wire 52Co-20Cr-10Ni-15W.pdfSAE-AMS5830C-2007 Nickel-Iron Alloy,Corrosion&Heat-Resistant,Welding Wire 12.5Cr-42.5Ni-6.0Mo-2.7Ti-0.015B-35Fe.pdfSAE-AMS5830C-2007 Nickel-Iron Alloy,Corrosion&Heat-Resistant,Welding Wire 12.5Cr-42.5Ni-6.0Mo-2.7Ti-0.015B-35Fe[P6].pdfSAE-AMS5857B-2007 Steel,Corrosion-Resistant,Bars&Wire 19Cr-10Ni (SAE-30304)High Yield Strength Solution Heat Treated&Cold Worked[P4].pdfSAE-AMS5869C-2008 Nickel Alloy.Corrosion&Heat-Resistant.Sheet.Strip.and Plate 62Ni-21.5Cr-9.0Mo-3.7Cb Solution Heat Treated.pdfSAE-AMS6257D-2007 Steel Bars,Forgings,and Tubing 1.6Si-0.82Cr-1.8Ni-0.40Mo-0.08V (0.40-0.44C)[P9].pdfSAE-AMS6260P-2007 Steel,Bars,Forgings,and Tubing 1.2Cr-3.2Ni-0.12Mo (0.07-0.13C) (SAE-9310)[P6].pdfSAE-AMS6267G-2007 Steel Bars,Forgings,and Tubing 1.2Cr-3.25Ni-0.12Mo (0.07-0.13C) (SAE-9310)[p6].pdfSAE-AMS6345B-2007 Steel,Sheet,Strip,and Plate 0.95Cr-0.20Mo (0.28-0.33C) (SAE-4130)[p7].pdf SAE-AMS6354F-2007 Steel,Sheet,Strip,and Plate 0.75Si-0.62Cr-0.20Mo-0.10Zr (0.10-0.17C)[P5].pdf SAE-AMS6359H-2007 Steel,Sheet,Strip,and Plate 0.80Cr-1.8Ni-0.25Mo (0.38-0.43C) (SAE-4340)[p6].pdfSAE-AMS6409C-2007 Steel,Bars,Forgings,and Tubing 0.80Cr-1.8Ni-0.25Mo (0.38-0.43C) (SAE-4340)[p8].pdfSAE-AMS6414K-2007 Steel,Bars,Forgings,and Tubing 0.80Cr-1.8Ni-0.25Mo (0.38-0.43C) (SAE-4340)[p9].pdfSAE-AMS6415S-2007 Steel,Bars,Forgings,and Tubing 0.80Cr-1.8Ni-0.25Mo (0.38-0.43C) (SAE-4340)[P8].pdfSAE-AMS6417F-2006 Steel,Bars,Forgings,and Tubing 1.6Si-0.82Cr-1.8Ni-0.40Mo-0.08V (0.38-0.43C)Consumable Electrode Vacuum Remelted.pdfSAE-AMS6440P-2007 Steel,Bars,Forgings,and Tubing 1.45Cr (0.93-1.05C) (SAE-52100) For Bearing Applications[p7].pdfSAE-AMS6454D-2007 Steel,Sheet,Strip,and Plate 1.8Ni-0.80Cr-0.25Mo (0.38-0.43C) (SAE-4340)Vacuum Consumable Electrode Remelted[p7].pdfSAE-AMS6501D-2007 Steel,Maraging,Welding Wire 18Ni-8.0Co-4.9Mo-0.40Ti-0.10Al Vacuum Induction Melted,Environment Controlled Packaging[p6].pdfSAE-AMS753-1998 Corrosion-Resistant Steel Parts Sampling,Inspection&Testing for Surface Passivation[P11].pdfSAE-AMS7721C-2007 Lead Alloy Sheet&Extrusions 93Pb-6.5Sb-0.50Sn ASFabricated[p5].pdfSAE-AMS7731C-2007 Gold Wire&Ribbon 99.97Au Annealed[p6].pdfSAE-AMS7881-2007 Tungsten Carbide-Cobalt Powder Agglomerated&Sintered[p5].pdfSAE-AMS7881-2007 Tungsten Carbide--Cobalt Powder Agglomerated&Sintered[P5].pdfSAE-AMS7882A-2007 Tungsten Carbide-Cobalt Chrome Powder Agglomerated&Sintered[p5].pdf SAE-AMS7882A-2007 Tungsten Carbide--Cobalt Chrome Powder Agglomerated&Sintered[P5].pdf SAE-AMS-A-22771A-2007 Aluminum Alloy Forgings,Heat Treated[p25].pdfSAE-AMS-C-5541A-2003 Chemical Conversion Coatings on Aluminum&Aluminum Alloys.pdfSAE-AMS-F-7190A-2007 Forging,Steel,For Aircraft_Aerospace Equipment&Special Ordnance Applications[p11].pdfSAE-AMS-H-6875-1998(R2006) Heat Treatment of Steel Raw Materials [P29].pdfSAE-AMS-I-23011A-2007 Iron-Nickel Alloys for Sealing to Glasses&Ceramic[P22].pdfSAE-AMS-M-7866A-2007 Molybdenum Disulfide,Technical,Lubrication Grade[p11].pdfSAE-AMS-QQ-A-200-13B-2007 Aluminum Alloy 7178,Bar,Rod,Shapes,Tube,and Wire,Extruded[p8].pdfSAE-AMS-QQ-A-200-14A-2007 Aluminum Alloy,Bar,Rod,Shapes,and Wire,Extruded,7178-T76 Improved Exfoliation Resistance[p8].pdfSAE-AMS-QQ-A-200-5A-2007 Aluminum Alloy 5086,Bar,Rod,Shapes,Tube,andWire,Extruded[p7].pdfSAE-AMS-QQ-A-200-7B-2007 Aluminum Alloy 5456,Bar,Rod,Shapes,Tube,and Wire,Extruded[p6].pdfSAE-AMS-QQ-A-200-9-1997 Aluminum Alloy 6063,Bar,Rod,Shapes,Tube,&Wire,Extruded.pdfSAE-AMS-QQ-A-250-10A-2007 Aluminum Alloy 5454,Plate&Sheet.pdfSAE-AMS-QQ-A-250-11A-2007 Aluminum Alloy 6061,Plate&Sheet.pdfSAE-AMS-QQ-A-250-12-2007 Aluminum Alloy 7075,Plate&Sheet.pdfSAE-AMS-QQ-A-250-13-2007 Aluminum Alloy Alclad 7075,Plate&Sheet.pdfSAE-AMS-QQ-A-250-14A-2007 Aluminum Alloy 7178,Plate&Sheet [p7].pdfSAE-AMS-QQ-A-250-15B-2007 Aluminum Alloy Alclad 7178,Plate&Sheet[p8].pdfSAE-AMS-QQ-A-250-21B-2007 Aluminum Alloy,7178-T76,Plate&Sheet Improved Exfoliation Resistant[p7].pdfSAE-AMS-QQ-A-250-22B-2007 Aluminum Alloy,7178-T76,Alclad Plate&Sheet,Improved Exfoliation Resistant[p10].pdfSAE-AMS-QQ-A-250-28B-2007 Aluminum Alloy,7011 Alclad 7178 Plate&Sheet[p14].pdfSAE-AMS-QQ-A-250-4A-2007 Aluminum Alloy 2024,Plate&Sheet..pdfSAE-AMS-QQ-A-250-5A-2007 Aluminum Alloy Alclad 2024,Plate&Sheet.pdfSAE-AMS-QQ-A-250-8A-1998 Aluminum Alloy 5052,Plate&Sheet.pdfSAE-AMS-QQ-A-250-9A-2006 Aluminum Alloy 5456,Plate&Sheet.pdfSAE-AMS-QQ-A-250A-2004 Aluminum&Aluminum Alloy,Plate&Sheet General Specification for.pdf SAE-AMS-QQ-A-367A-2007 Aluminum Alloy Forgings[p29].pdfSAE-AMS-S-13165 Issued NOV1997 Shot Peening of Metal Parts[P27].pdfSAE-AMS-W-6858A-2000 Welding,Resistance Spot&Seam[P46].pdfSAE-ARP1232B-2001 Gland Design,Elastomeric O-Ring Seals,Static Radial..pdfSAE-ARP1420B-2002 Gas Turbine Engine Inlet Flow Distortion Guidelines.pdfSAE-ARP1420B-2002 Gas Turbine Engine Inlet Flow Distortion Guidelines[P24].pdfSAE-ARP1755B-2000 Effect of Cleaning Agents on Aircraft Engine Materials Stock Loss Test Method.PDFSAE-ARP1962A-1995 TRAINING&APPROVAL OF HEAT-TREA TING PERSONNEL.PDFSAE-ARP4191-2003 C Gas Turbine Engine Performance Presentation[P9].pdfSAE-ARP4191C-2003 Gas Turbine Engine Performance PresentationDigital Computer Programs Using FORTRAN 77.pdfSAE-ARP4191C-2003Gas Turbine Engine Performance Presentation [P9].pdfSAE-ARP4754-1996 ConsiderationsHighly-Integrated or Complex Aircraft Systems[P101].pdfSAE-ARP5316B-2002 Storage of Elastomer Seals&Seal Assemblies Which Include an Elastomer Element Prior to Hardware Assembly.pdfSAE-ARP5580-2001 非机动车用的故障模式和效果分析的推荐实施规范.pdfSAE-ARP598C-2003 Aerospace Microscopic Sizing&Counting of Particulate Contamination for Fluid Power Systems[P16].pdfSAE-AS122026A THRU AS122075A-2007 WASHER-LOCK,SPRING,CADMI[p3].pdfSAE-AS123601 THRU AS123750B-2007 RIVET,SOLID,100 FLUSH HEA[p3].pdfSAE-AS1241-1997 Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft.pdfSAE-AS14101-1998 低速自调心自润滑关节轴承.pdfSAE-AS14153B-2007 CIRCUIT BREAKER-AIRCRAFT,TRIP-FREE,[P3].pdfSAE-AS14154B-2007 Circuit Breaker-Aircraft,Trip-Free,Push-P[P3].pdfSAE-AS15001B-2007 FITTING,LUBRICATION,HYDRAULIC,SURFACE CHEC[P3].pdfSAE-AS15002B-2007 FITTING,LUBRICATION,HYDRAULIC,SURFACE CHEC[P3].pdfSAE-AS15003B-2007 FITTING,LUBRICATION,HYDRAULIC,SURFACE CHEC[P3].pdfSAE-AS15005B-2007 FITTING,LUBRICATION,HYDRAULIC,THROA T OR SU[P3].pdfSAE-AS15006B-2007 FITTING,LUBRICATION,HYDRAULIC,LEAKPROOF,1_8 PIPE THREADS[P3].pdfSAE-AS155001 THRU AS155300A-2007 STUD,STEPPED,2 DIA ENGAGEME[p3].pdfSAE-AS155301 THRU AS155600A-2007 STUD,STEPPED,2 DIA ENGAGEME[p3].pdfSAE-AS155901 THRU AS156200A-2007 STUD,STEPPED,2 DIA ENGAGEMENT,CADMIUM PLATED,STEEL UNS G87400,[p2].pdfSAE-AS158901 THRU AS159200A-2007 STUD,STEPPED,NECKED,1.5 DIA ENGAGEMENT,CADMIUM PLATED,STEEL[P3].pdfSAE-AS162501 THRU AS162800A-2007 STUD,STEPPED,DRILLED,NECKED,2 DIA ENGAGEMENT,CADMIUM PLATED,STEEL[p3].pdfSAE-AS17108A-2008 (R) bearing,ball,annular,primarily for aircraft generators&motor-generators,wide cartridge,type ii.pdfSAE-AS22759-10-2000 wire,electrical,fluoropolymer-insulated,extruded tfe,nickel-coated copper conductor,1000 volt.pdfSAE-AS22759-86B-2007 wire,electrical,polytetrafluoroethylene polyimide insulated,normal weight,silver coated,copper conductor,200 °c,600 volts.pdfSAE-AS22759-87B-2007 wire,electrical,polytetrafluoroethylene-polyimide insulated,normal weight,nickel coated,copper conductor,260 °c,600 volts.pdfSAE-AS22759-89B-2007 Wire,Electrical,Polytetrafluoroethylene-Polyimide Insulated,Normal Weight,Silver Coated,High Strength or Ultra High Strength Copper Alloy,200-mDC,600 V olts.pdf SAE-AS23190-1-1999(R2006) Straps,Clamps,&Mounting Hardware,Plastic for Cable Harness Tying&Support Clamp,Loop,Nylon,Adjustable,Wire Support[P5].pdfSAE-AS23190-1998 Straps,Clamps,&Mounting Hardware,Plastic&Metal for Cable Harness Tying&Support-FSC 5975[P42].pdfSAE-AS23190-2-1998(R2003) Straps,Clamps,Plastic&Metal,&Mounting Hardware,Plastic for Cable Harness Tying&Support Clamp,Loop,Metal[P9].pdfSAE-AS23190-3-2008 Straps,Clamps,&Mounting Hardware,Plastic&Metal for Cable Harness Tying&Support Strap,Tie down[P3].pdfSAE-AS25244-2007 CIRCUIT BREAKER,TRIP-FREE,PUSH-PULL,5 THRU [P6].pdfSAE-AS25361A-2007 CIRCUIT BREAKER -AIRCRAFT,TRIP-FREE,PUSH-PULL,50 THRU 100 AMP,TYPE I,[P3].pdfSAE-AS3086A-2007 STUD-STRAIGHT,KEY LOCKED,CADMIUM PLA TED,S[p2].pdfSAE-AS3087A-2007 STUD-STRAIGHT,KEY LOCKED,CADMIUM PLA TED,S[P3].pdfSAE-AS3088A-2007 STUD,STRAIGHT,KEY LOCKED,CADMIUM PLA TED,ST[P3].pdfSAE-AS3089A-2007 STUD,STRAIGHT,KEY LOCKED,CADMIUM PLA TED,ST[P3].pdfSAE-AS33514A-2007 Fitting End,Standard Dimensions for Flareles[P3].pdfSAE-AS33515A-2007 FITTING END,STANDARD DIMENSIONS FOR BULKHEAD[P3].pdfSAE-AS39029-19A-2007 CONTACTS,ELECTRICAL CONNECTOR,PIN,CRIMP[P5].pdfSAE-AS39029-21A-2007 CONTACTS,ELECTRICAL CONNECTOR,SOCKET,CR[P5].pdf。
ams5662m标准
ams5662m标准
经过查阅，AMS5662M是一种关于高温合金钛合金Ti-6Al-2Sn-4Zr-2Mo（UNS 号R56620）的标准。
它是由Society of Automotive Engineers (SAE) 和全球航空材料供应商协会 (Global Aerospace Materials Suppliers, GAMPS) 共同制定的标准。
AMS5662M涵盖了对Ti-6Al-2Sn-4Zr-2Mo钛合金在固溶热处理和变形加工状态下的化学成分、物理性质、机械性能和表面质量等方面的要求。
该标准还包括了热处理和冷加工后的材料的可接受的缺陷和表面缺陷的限制。
通过遵循AMS5662M标准，制造商可以确保生产出符合规范的Ti-6Al-2Sn-4Zr-2Mo钛合金材料，以满足航空航天和其他高温应用领域的要求。
该标准对材料的性能和质量进行了严格的规定，有助于确保材料具有良好的可靠性、耐高温性和耐腐蚀性。
AMS5662M标准是经过定期修订和更新的，所以建议用户在实际应用中使用最新版本的标准。
此外，为了确保最佳结果，建议与相关的标准机构或认证机构进行进一步的确认和咨询。
高温合金牌号 国标
高温合金牌号国标高温合金是一种在高温环境下具有良好抗氧化性、热疲劳性、蠕变性和耐磨性的合金。
它广泛应用于航空航天、电力、石油化工、核工业以及其他工业领域。
高温合金的种类繁多，根据不同的成分和性能，可以分为以下几类：1.镍基高温合金：以镍为主要基体元素，具有优良的抗氧化性、热疲劳性和蠕变性。
常见的镍基高温合金有IN718、IN738、IN939等。
2.钴基高温合金：以钴为主要基体元素，具有较高的熔点、良好的抗氧化性和耐磨性。
常见的钴基高温合金有CoCrAlY、CoNiCrAlY等。
3.铁基高温合金：以铁为主要基体元素，具有较高的热疲劳性、蠕变性和抗氧化性。
常见的铁基高温合金有Fecralloy、FeNiCrAlY等。
4.金属间化合物高温合金：具有高熔点、高抗氧化性和高蠕变性。
常见的金属间化合物高温合金有Ni3Al、Ni3(Al,Ti)等。
在我国，高温合金牌号按照GB/T 1500-2009《高温合金和耐热钢》进行分类。
根据国标，高温合金牌号分为以下几类：1.镍基高温合金：以Ni-Fe、Ni-Cr为主要成分，如GH30、GH40、GH50等。
2.钴基高温合金：以Co-Cr、Co-Ni为主要成分，如CoCrAlY、CoNiCrAlY等。
3.铁基高温合金：以Fe-Cr、Fe-Ni为主要成分，如Fecralloy、FeNiCrAlY等。
4.金属间化合物高温合金：以Ni3Al、Ni3(Al,Ti)为主要成分，如IN736、IN929等。
在选择高温合金牌号时，需根据实际应用场景和性能要求进行挑选。
以下为国标高温合金牌号选择建议：1.高温抗氧化性：选用Ni基和Co基高温合金。
2.高温蠕变性：选用Ni基和铁基高温合金。
3.高温热疲劳性：选用Ni基、Co基和铁基高温合金。
4.耐磨性：选用Co基和金属间化合物高温合金。
5.焊接性能：选用Ni基和铁基高温合金。
综上，高温合金在各种工业领域具有广泛应用，国标对其进行分类，便于选用。
镍基高温合金
少，提高了组织长期稳定性等。这类合金已在美国获得
实际应用。
• 应用 镍基铸造高温合金用于飞机、船舶、工业和车
辆用燃气轮机的最关键的高温部件，如涡轮机叶片、
导向叶片和整体涡轮等。
四、生产工艺
• 冶炼方面：为了获得更纯净化的钢水，减 低气体含量与有害元素含量；同时由于部分合 金中有易氧化元素如Al，Ti等存在，非真空方 式冶炼难以控制；更是为了获得更好的热塑性， 镍基耐热合金，通常采用真空感应炉熔炼，甚 至用真空感应冶炼加真空自耗炉或电渣炉重熔 方式进行生产。
为了满足舰船和工业燃气轮机的需要，60年 代以来还发展出一批抗热腐蚀性能较好、组织 稳定的高铬镍基合金。
在从40年代初到70年代末大约40年的时间内， 镍基合金的工作温度从 700℃提高到1100℃， 平均每年提高10℃左右。
二、分类
• 高温合金材料按制造工艺，可分为变形高温合金、铸
造高温合金、粉末冶金高温合金和发散冷却高温合金。
• 以镍为主要基体成分的变形高温合金。镍基变形高温 合金以汉语拼音字母“GH” 加序号表示，如GH36、
GH49、GH141等。它可采用常规的锻、轧和挤压等
冷、热变形手段加工成材。 • 按强化方式可分为固溶强化镍基变形高温合金，弱时
效强化镍基变形高温合金和强时效强化镍基变形高温
合金3类。
• 用途：镍基变形高温合金广泛地用来制造航空喷气发
工艺，如钢锭直接轧制、钢锭包套直接轧制和包套镦饼等
新工艺。也采用加镁微合金化和弯曲晶界热处理工艺来提 高塑性。
镍基铸造高温合金 （cast nickel - base superalloy ）
• 以镍为主要成分的铸造高温合金，以“K”加序号表示，
如K1、K2等。 • 随着使用温度和强度的提高，高温合金的合金化程度 越来越高，热加工成形越来越困难，必须采用铸造工 艺进行生产。另外，采用冷却技术的空心叶片的内部 复杂型腔，只能采用精密铸造工艺才能生产。这样， 镍基变形高温合金就转化为镍基铸造高温合金。
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fx or .
ASTM E 8 ASTM E 8M ASTM E 10
z ASTM E 21
ASTM E 103 ASTM E 112
.b ASTM E 139
ASTM E 292 ASTM E 354
Tension Testing of Metallic Materials Tension Testing of Metallic Materials (Metric) Brinell Hardness of Metallic Materials Elevated Temperature Tension Tests of Metallic Materials Rapid Indentation Hardness Testing of Metallic Materials Determining Average Grain Size Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials Conducting Time-for-Rupture Notch Tension Tests of Materials Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys
AMS 2261 AMS 2269 AMS 2371
m AMS 2374
AMS 2750
o AMS 2806 .c AMS 2808
AMS 7490
Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings Pyrometry Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys Identification, Forgings Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels, AusteniticType Iron, Nickel, or Cobalt Alloys, or Precipitation-Hardenable Alloys
ww SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely w voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”
3. TECHNICAL REQUIREMENTS:
w 3.1 Composition:
Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods
w in accordance with ASTM E 354, by spectrochemical methods, by the methods of ARP1313 for lead, wbismuth, and selenium, or by other analytical methods acceptable to purchaser.
Email: custsvc@
Copyright SSAAE EInteWrnEatiBonaAl DDRESS:
Provided by IHS under license with SAE
Licensee=Messier Dowty/5905381001
AEROSPACE
AMS 5662M
MATERIAL
Issued
SEP 1965
SPECIFICATION Revised JUL 2004
Superseding AMS 5662L
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe
m Consumable Electrode or Vacuum Induction Melted
1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable
(Composition similar to UNS N07718)
o 1. SCOPE: .c 1.1 Form:
Element
Carbon Manganese
m Silicon
Phosphorus Sulfur
o Chromium
SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.
No reproduction or networking permitted without license from IHS
Not for Resale, 11/27/2006 20:5
AMS 5662M
2.1 SAE Publications:
Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or .
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Copyright SAE International Provided by IHS under license with SAE No reproduction or networking permitted without license from IHS
w 1.2 Application: These products have been used typically for parts requiring high resistance to creep and stressfx rupture up to 1300 °F (704 °C) and oxidation resistance up to 1800 °F (982 °C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.
TO PLACE A DOCUMENT ORDER: Tel:
877-606-7323 (inside USA and Canada)
Tel:
724-776-4970 (outside USA)
Fax:
724-776-0790
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This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.